Range / Endurance Profile - Cirrus SR22 Pilot Operating Handbook

Cirrus Design
SR22

Range / Endurance Profile

Conditions:
• Weight ..................................................3600 LB for Climb, Avg 3400 LB for Cruise
• Temperature ....................................................................................... Standard Day
• Winds ............................................................................................................... Zero
• Mixture ..............................................................................................Best Economy
• Total Fuel.................................................................................................92 Gallons
Fuel Remaining For Cruise is equal to 92.0 gallons usable, less climb fuel,
less 9.8 gallons for 45 minutes IFR reserve fuel at 65% power (ISA @ 10,000
ft PA), less descent fuel, less fuel used prior to takeoff.
Range and endurance shown includes descent to final destination at
approximately 178 KIAS and 500 fpm.
Range is decreased by 5% if nose wheel pant and fairings removed.
Range is decreased by 15% if nose and main wheel pants and fairings
removed.
Aircraft with optional air conditioning system - Range is decreased by 1%. For
maximum range the air-conditioner should be off.
Aircraft with optional Enhanced Vision System: range is decreased by ½%.
75% POWER
Press Climb
Alt Fuel
FT Gal
SL 0.0
2000 0.7
4000 1.5
6000 2.3
8000 3.1
P/N 13772-004 P/N 13772-004
Original Issue
Fuel Airspeed
Remaining
For Cruise
Gal KTAS
81.2 166
79.3 170
77.4 173
75.5 177
73.5 180
• Note •
Fuel Endurance
Flow
GPH Hours
17.8 4.6
17.8 4.5
17.8 4.5
17.8 4.4
17.8 4.4
Section 5
Performance Data
Mixture: Best Power
Range Specific
Range
NM Nm/Gal
758 9.3
769 9.6
780 9.8
792 10.0
804 10.3
5-25 5-25